Sunday, August 29, 2010

Cryosat

 2010-013A


The two main stages put the payload module on a suborbital trajectory; the final stage MIRV bus then performs the low-thrust orbit insertion burn, dragging the payload behind it into a 710 x 726 km x 92.0 deg orbit. The final stage ended up in a higher orbit of 716 x 1119 km.


Cryosat
 

DateTimeEventOrbit  

2010 Apr 8  1357:04  Launch by Dnepr  KB LC109/95 
  T+1:50 Stage 1 sep 
  T+5:09 GO 
  T+5:54 St 2 sep 
 1401 T+5:55? DU on 
 1412? Plume shield sep 
 1413 T+16:28 Satellite separation 
 1413? DS MECO 

Payload:

  • SIRAL SAR Ku-band interferometric radar altimeter 1 and 2

  • DORIS receiver

  • Laser retroreflectors

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